DEVICE FOR CONFIRMING THE ENGINE THRUST OF AN AIRCRAFT
First Claim
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1. A device for confirming the thrust of the engines of an aircraft while it is running on the ground, upon the take-off phase thereof, such a device comprising:
- at least one display screen (2) in the cockpit permanently displaying at least one control parameter of each engine allowing to check the thrust delivered by one of them;
an operating logic unit (14) for each engine, receiving at least information on said control parameter of said engine when said thrust is reached, on the take-off mode position of the throttle lever corresponding to said engine and on the ground position of said aircraft; and
a warning indicator connected at the outlet of said logic unit and able to display, at the level of said cockpit, thrust confirmation information when said information received by said logic unit is validated.
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Abstract
A device for confirming the engine thrust of an aircraft is disclosed. The device, via an operating logic unit (14) of each engine processing different information, including a warning indicator (15) connected to the unit (14) delivers or not thrust confirmation information at the level of the cockpit.
17 Citations
10 Claims
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1. A device for confirming the thrust of the engines of an aircraft while it is running on the ground, upon the take-off phase thereof, such a device comprising:
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at least one display screen (2) in the cockpit permanently displaying at least one control parameter of each engine allowing to check the thrust delivered by one of them; an operating logic unit (14) for each engine, receiving at least information on said control parameter of said engine when said thrust is reached, on the take-off mode position of the throttle lever corresponding to said engine and on the ground position of said aircraft; and a warning indicator connected at the outlet of said logic unit and able to display, at the level of said cockpit, thrust confirmation information when said information received by said logic unit is validated. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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Specification